Source code for pyNastran.op2.tables.oes_stressStrain.real.oes_bars

from typing import List

import numpy as np
from numpy import zeros, searchsorted, ravel

from pyNastran.utils.numpy_utils import integer_types
from pyNastran.op2.result_objects.op2_objects import get_times_dtype
from pyNastran.op2.tables.oes_stressStrain.real.oes_objects import (
    StressObject, StrainObject, OES_Object, oes_data_code)
from pyNastran.f06.f06_formatting import write_floats_13e, _eigenvalue_header

ELEMENT_NAME_TO_ELEMENT_TYPE = {
    'CBAR' : 34,
}
#oxx = 0. # max from bending and axial
#txz = 1. # from transverse shear; txz=Vz/(Kz*A)
#txy = 1. # from transverse shear; txy=Vz/(Ky*A)
#t = 2. # from torsional stress; t=T*C/J
#ovm = (oxx**2 + 3 * (txy**2 + txz**2 + t**2))**0.5

[docs]class RealBarArray(OES_Object): def __init__(self, data_code, is_sort1, isubcase, dt): OES_Object.__init__(self, data_code, isubcase, apply_data_code=False) #self.code = [self.format_code, self.sort_code, self.s_code] #self.ntimes = 0 # or frequency/mode #self.ntotal = 0 self.ielement = 0 self.nelements = 0 # result specific #if not is_sort1: #raise NotImplementedError('SORT2') #assert dt is not None #self.add = self.add_sort2 #self.add_new_eid = self.add_new_eid_sort2 #self.addNewNode = self.addNewNodeSort2 @property def is_real(self) -> bool: return True @property def is_complex(self) -> bool: return False @property def nnodes_per_element(self) -> int: return 1 def _reset_indices(self): self.itotal = 0 self.ielement = 0
[docs] @classmethod def add_static_case(cls, table_name, element_name, element, data, isubcase, is_sort1=True, is_random=False, is_stress=True, is_msc=True, random_code=0, title='', subtitle='', label=''): analysis_code = 1 # static data_code = oes_data_code(table_name, analysis_code, is_sort1=is_sort1, is_random=is_random, random_code=random_code, title=title, subtitle=subtitle, label=label, is_msc=is_msc) data_code['lsdvmns'] = [0] # TODO: ??? data_code['data_names'] = [] # I'm only sure about the 1s in the strains and the # corresponding 0s in the stresses. if is_stress: data_code['stress_bits'] = [0, 0, 0, 0] data_code['s_code'] = 0 else: data_code['stress_bits'] = [0, 1, 0, 1] data_code['s_code'] = 1 # strain? element_type = ELEMENT_NAME_TO_ELEMENT_TYPE[element_name] data_code['element_name'] = element_name data_code['element_type'] = element_type data_code['load_set'] = 1 ntimes = data.shape[0] nnodes = data.shape[1] dt = None obj = cls(data_code, is_sort1, isubcase, dt) obj.element = element obj.data = data obj.ntimes = ntimes obj.ntotal = nnodes obj._times = [None] obj.is_built = True return obj
def _get_msgs(self): raise NotImplementedError('%s needs to implement _get_msgs' % self.__class__.__name__)
[docs] def get_headers(self): raise NotImplementedError('%s needs to implement get_headers' % self.__class__.__name__)
[docs] def build(self): """sizes the vectorized attributes of the RealBarArray""" #print("self.ielement =", self.ielement) #print('ntimes=%s nelements=%s ntotal=%s' % (self.ntimes, self.nelements, self.ntotal)) assert self.ntimes > 0, 'ntimes=%s' % self.ntimes assert self.nelements > 0, 'nelements=%s' % self.nelements assert self.ntotal > 0, 'ntotal=%s' % self.ntotal #if self.element_type == 34: #nnodes_per_element = 1 #else: #raise NotImplementedError(self.element_type) self.itime = 0 self.ielement = 0 self.itotal = 0 #self.ntimes = 0 #self.nelements = 0 self.is_built = True #print("***name=%s type=%s nnodes_per_element=%s ntimes=%s nelements=%s ntotal=%s" % ( #self.element_name, self.element_type, nnodes_per_element, self.ntimes, self.nelements, self.ntotal)) dtype, idtype, fdtype = get_times_dtype(self.nonlinear_factor, self.size) _times = zeros(self.ntimes, dtype=dtype) element = zeros(self.ntotal, dtype=idtype) #[s1a, s2a, s3a, s4a, axial, smaxa, smina, MS_tension, # s1b, s2b, s3b, s4b, sminb, sminb, MS_compression] data = zeros((self.ntimes, self.ntotal, 15), dtype=fdtype) if self.load_as_h5: #for key, value in sorted(self.data_code.items()): #print(key, value) group = self._get_result_group() self._times = group.create_dataset('_times', data=_times) self.element = group.create_dataset('element', data=element) self.data = group.create_dataset('data', data=data) else: self._times = _times self.element = element self.data = data
[docs] def build_dataframe(self): """creates a pandas dataframe""" import pandas as pd headers = self.get_headers() if self.nonlinear_factor not in (None, np.nan): column_names, column_values = self._build_dataframe_transient_header() data_frame = self._build_pandas_transient_elements( column_values, column_names, headers, self.element, self.data) #data_frame = pd.Panel(self.data, items=column_values, major_axis=self.element, minor_axis=headers).to_frame() #data_frame.columns.names = column_names #data_frame.index.names = ['ElementID', 'Item'] else: data_frame = pd.DataFrame(self.data[0], columns=headers, index=self.element) data_frame.index.name = 'ElementID' data_frame.columns.names = ['Static'] self.data_frame = data_frame
def __eq__(self, table): # pragma: no cover assert self.is_sort1 == table.is_sort1 self._eq_header(table) if not np.array_equal(self.data, table.data): msg = 'table_name=%r class_name=%s\n' % (self.table_name, self.__class__.__name__) msg += '%s\n' % str(self.code_information()) ntimes = self.data.shape[0] i = 0 if self.is_sort1: for itime in range(ntimes): for ieid, eid, in enumerate(self.element): t1 = self.data[itime, ieid, :] t2 = table.data[itime, ieid, :] (axial_stress1, equiv_stress1, total_strain1, effective_plastic_creep_strain1, effective_creep_strain1, linear_torsional_stress1) = t1 (axial_stress2, equiv_stress2, total_strain2, effective_plastic_creep_strain2, effective_creep_strain2, linear_torsional_stress2) = t2 if not np.allclose(t1, t2): #if not np.array_equal(t1, t2): msg += '%s\n (%s, %s, %s, %s, %s, %s)\n (%s, %s, %s, %s, %s, %s)\n' % ( eid, axial_stress1, equiv_stress1, total_strain1, effective_plastic_creep_strain1, effective_creep_strain1, linear_torsional_stress1, axial_stress2, equiv_stress2, total_strain2, effective_plastic_creep_strain2, effective_creep_strain2, linear_torsional_stress2) i += 1 if i > 10: print(msg) raise ValueError(msg) else: raise NotImplementedError(self.is_sort2) if i > 0: print(msg) raise ValueError(msg) return True
[docs] def add_new_eid_sort1(self, dt, eid, s1a, s2a, s3a, s4a, axial, smaxa, smina, MSt, s1b, s2b, s3b, s4b, smaxb, sminb, MSc): assert isinstance(eid, integer_types) self._times[self.itime] = dt self.element[self.itotal] = eid self.data[self.itime, self.itotal, :] = [s1a, s2a, s3a, s4a, axial, smaxa, smina, MSt, s1b, s2b, s3b, s4b, smaxb, sminb, MSc] self.itotal += 1 self.ielement += 1
#def add_sort1(self, dt, eid, nodeID, fd, oxx, oyy, txy, angle, majorP, minorP, ovm): #assert eid is not None #msg = "i=%s dt=%s eid=%s nodeID=%s fd=%g oxx=%g oyy=%g \ntxy=%g angle=%g major=%g minor=%g ovmShear=%g" % ( #self.itotal, dt, eid, nodeID, fd, oxx, oyy, txy, angle, majorP, minorP, ovm) ##print(msg) #if isinstance(nodeID, str): #nodeID = 0 ##assert isinstance(nodeID, integer_types), nodeID #self.element_node[self.itotal, :] = [eid, nodeID] #self.data[self.itime, self.itotal, :] = [fd, oxx, oyy, txy, angle, majorP, minorP, ovm] #self.itotal += 1
[docs] def get_stats(self, short=False) -> List[str]: if not self.is_built: return [ '<%s>\n' % self.__class__.__name__, ' ntimes: %i\n' % self.ntimes, ' ntotal: %i\n' % self.ntotal, ] nelements = self.ntotal ntimes = self.ntimes unused_ntotal = self.ntotal nelements = self.ntotal msg = [] if self.nonlinear_factor not in (None, np.nan): # transient msg.append(' type=%s ntimes=%i nelements=%i\n' % (self.__class__.__name__, ntimes, nelements)) ntimes_word = 'ntimes' else: msg.append(' type=%s nelements=%i\n' % (self.__class__.__name__, nelements)) ntimes_word = '1' headers = self.get_headers() n = len(headers) assert n == self.data.shape[2], 'nheaders=%s shape=%s' % (n, str(self.data.shape)) msg.append(' data: [%s, ntotal, %i] where %i=[%s]\n' % (ntimes_word, n, n, str(', '.join(headers)))) msg.append(' data.shape = %s\n' % str(self.data.shape).replace('L', '')) msg.append(' element.shape = %s\n' % str(self.element.shape).replace('L', '')) msg.append(' element type: %s\n' % self.element_name) msg += self.get_data_code() return msg
[docs] def get_element_index(self, eids): # elements are always sorted; nodes are not itot = searchsorted(eids, self.element) #[0] return itot
[docs] def eid_to_element_node_index(self, eids): ind = ravel([searchsorted(self.element == eid) for eid in eids]) #ind = searchsorted(eids, self.element) #ind = ind.reshape(ind.size) #ind.sort() return ind
[docs] def write_f06(self, f06_file, header=None, page_stamp='PAGE %s', page_num=1, is_mag_phase=False, is_sort1=True): if header is None: header = [] msg = self._get_msgs() ntimes = self.data.shape[0] eids = self.element #print('CBAR ntimes=%s ntotal=%s' % (ntimes, ntotal)) for itime in range(ntimes): dt = self._times[itime] header = _eigenvalue_header(self, header, itime, ntimes, dt) f06_file.write(''.join(header + msg)) s1a = self.data[itime, :, 0] s2a = self.data[itime, :, 1] s3a = self.data[itime, :, 2] s4a = self.data[itime, :, 3] axial = self.data[itime, :, 4] smaxa = self.data[itime, :, 5] smina = self.data[itime, :, 6] MSt = self.data[itime, :, 7] s1b = self.data[itime, :, 8] s2b = self.data[itime, :, 9] s3b = self.data[itime, :, 10] s4b = self.data[itime, :, 11] smaxb = self.data[itime, :, 12] sminb = self.data[itime, :, 13] MSc = self.data[itime, :, 14] for (eid, s1ai, s2ai, s3ai, s4ai, axiali, smaxai, sminai, MSti, s1bi, s2bi, s3bi, s4bi, smaxbi, sminbi, MSci) in zip( eids, s1a, s2a, s3a, s4a, axial, smaxa, smina, MSt, s1b, s2b, s3b, s4b, smaxb, sminb, MSc): vals = [s1ai, s2ai, s3ai, s4ai, axiali, smaxai, sminai, MSti, s1bi, s2bi, s3bi, s4bi, smaxbi, sminbi, MSci] vals2 = write_floats_13e(vals) [s1ai, s2ai, s3ai, s4ai, axiali, smaxai, sminai, MSti, s1bi, s2bi, s3bi, s4bi, smaxbi, sminbi, MSci] = vals2 f06_file.write('0%8i %-13s %-13s %-13s %-13s %-13s %-13s %-13s %s\n' ' %8s %-13s %-13s %-13s %-13s %-13s %-13s %-13s %s\n' % (eid, s1ai, s2ai, s3ai, s4ai, axiali, smaxai, sminai, MSti, '', s1bi, s2bi, s3bi, s4bi, '', smaxbi, sminbi, MSci)) f06_file.write(page_stamp % page_num) page_num += 1 if self.nonlinear_factor in (None, np.nan): page_num -= 1 return page_num
[docs] def write_op2(self, op2, op2_ascii, itable, new_result, date, is_mag_phase=False, endian='>'): """writes an OP2""" import inspect from struct import Struct, pack frame = inspect.currentframe() call_frame = inspect.getouterframes(frame, 2) op2_ascii.write('%s.write_op2: %s\n' % (self.__class__.__name__, call_frame[1][3])) if itable == -1: self._write_table_header(op2, op2_ascii, date) itable = -3 #if isinstance(self.nonlinear_factor, float): #op2_format = '%sif' % (7 * self.ntimes) #raise NotImplementedError() #else: #op2_format = 'i21f' #s = Struct(op2_format) eids = self.element eids_device = eids * 10 + self.device_code # table 4 info #ntimes = self.data.shape[0] #nnodes = self.data.shape[1] nelements = self.data.shape[1] # 21 = 1 node, 3 principal, 6 components, 9 vectors, 2 p/ovm #ntotal = ((nnodes * 21) + 1) + (nelements * 4) ntotali = self.num_wide ntotal = ntotali * nelements #print('shape = %s' % str(self.data.shape)) #assert self.ntimes == 1, self.ntimes op2_ascii.write(' ntimes = %s\n' % self.ntimes) #fmt = '%2i %6f' #print('ntotal=%s' % (ntotal)) #assert ntotal == 193, ntotal if self.is_sort1: struct1 = Struct(endian + b'i 15f') else: raise NotImplementedError('SORT2') op2_ascii.write('nelements=%i\n' % nelements) for itime in range(self.ntimes): self._write_table_3(op2, op2_ascii, new_result, itable, itime) # record 4 #print('stress itable = %s' % itable) itable -= 1 header = [4, itable, 4, 4, 1, 4, 4, 0, 4, 4, ntotal, 4, 4 * ntotal] op2.write(pack('%ii' % len(header), *header)) op2_ascii.write('r4 [4, 0, 4]\n') op2_ascii.write('r4 [4, %s, 4]\n' % (itable)) op2_ascii.write('r4 [4, %i, 4]\n' % (4 * ntotal)) s1a = self.data[itime, :, 0] s2a = self.data[itime, :, 1] s3a = self.data[itime, :, 2] s4a = self.data[itime, :, 3] axial = self.data[itime, :, 4] smaxa = self.data[itime, :, 5] smina = self.data[itime, :, 6] MSt = self.data[itime, :, 7] s1b = self.data[itime, :, 8] s2b = self.data[itime, :, 9] s3b = self.data[itime, :, 10] s4b = self.data[itime, :, 11] smaxb = self.data[itime, :, 12] sminb = self.data[itime, :, 13] MSc = self.data[itime, :, 14] for (eid_device, s1ai, s2ai, s3ai, s4ai, axiali, smaxai, sminai, MSti, s1bi, s2bi, s3bi, s4bi, smaxbi, sminbi, MSci) in zip( eids_device, s1a, s2a, s3a, s4a, axial, smaxa, smina, MSt, s1b, s2b, s3b, s4b, smaxb, sminb, MSc): data = [eid_device, s1ai, s2ai, s3ai, s4ai, axiali, smaxai, sminai, MSti, s1bi, s2bi, s3bi, s4bi, smaxbi, sminbi, MSci] op2_ascii.write(' eid_device=%s data=%s\n' % (eid_device, str(data))) op2.write(struct1.pack(*data)) itable -= 1 header = [4 * ntotal,] op2.write(pack('i', *header)) op2_ascii.write('footer = %s\n' % header) new_result = False return itable
[docs]class RealBarStressArray(RealBarArray, StressObject): def __init__(self, data_code, is_sort1, isubcase, dt): RealBarArray.__init__(self, data_code, is_sort1, isubcase, dt) StressObject.__init__(self, data_code, isubcase)
[docs] def get_headers(self) -> List[str]: headers = ['s1a', 's2a', 's3a', 's4a', 'axial', 'smaxa', 'smina', 'MS_tension', 's1b', 's2b', 's3b', 's4b', 'smaxb', 'sminb', 'MS_compression'] return headers
def _get_msgs(self): if self.element_type == 34: pass else: raise NotImplementedError(self.element_type) msg = [ ' S T R E S S E S I N B A R E L E M E N T S ( C B A R )\n', ' ELEMENT SA1 SA2 SA3 SA4 AXIAL SA-MAX SA-MIN M.S.-T\n', ' ID. SB1 SB2 SB3 SB4 STRESS SB-MAX SB-MIN M.S.-C\n', ] return msg
[docs]class RealBarStrainArray(RealBarArray, StrainObject): def __init__(self, data_code, is_sort1, isubcase, dt): RealBarArray.__init__(self, data_code, is_sort1, isubcase, dt) StrainObject.__init__(self, data_code, isubcase)
[docs] def get_headers(self) -> List[str]: headers = ['e1a', 'e2a', 'e3a', 'e4a', 'axial', 'emaxa', 'emina', 'MS_tension', 'e1b', 'e2b', 'e3b', 'e4b', 'emaxb', 'eminb', 'MS_compression'] return headers
def _get_msgs(self): if self.element_type == 34: pass else: raise NotImplementedError(self.element_type) msg = [ ' S T R A I N S I N B A R E L E M E N T S ( C B A R )\n', ' ELEMENT SA1 SA2 SA3 SA4 AXIAL SA-MAX SA-MIN M.S.-T\n', ' ID. SB1 SB2 SB3 SB4 STRAIN SB-MAX SB-MIN M.S.-C\n', ] return msg